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Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory
Authors:Email author" target="_blank">A?V?GorelovEmail author  E?I?Nikolaev  I?N?Sidorov
Institution:1.Chistopol branch “Vostok”,Tupolev Kazan National Research Technical University,Tatarstan,Russia;2.PAO Kazan Helicopters,Tatarstan,Russia;3.Tupolev Kazan National Research Technical University,Tatarstan,Russia
Abstract:Safety factors of the Ansat helicopter main rotor blade are determined in the root section at various flight modes with taking into account the possible damages.
Keywords:
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